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Mach number
Results: 151

#	Item
111	REPORT 1389 CHARACTERISTICS OF THE LANGLEY 8-FOOT TRA.NSONIC TUNNEL WITH SLOTTED TEST SECTION ‘ By RAY H. WRIGHT, VIEGILS. RITCEIIE, Add to Reading List Source URL: crgis.ndc.nasa.gov Language: English - Date: 2009-12-07 16:09:08 Fluid mechanics Aerospace engineering Mach wave Mach number Shock wave Wind tunnel Bow shock Subsonic and transonic wind tunnel Aerodynamics Fluid dynamics Dynamics
112	Acoustic Radiation from a Submerged Pile during Pile Driving Per G. Reinhall1 and Peter H. Dahl1,2 1 Dept. of Mechanical Engineering Add to Reading List Source URL: www.wsdot.wa.gov Language: English - Date: 2014-08-13 08:07:41 Fluid dynamics Physics Civil engineering Building engineering Pile driver Deep foundation Underwater acoustics Speed of sound Mach number Geotechnical engineering Geology Aerodynamics
113	NewsRelease National Aeronautics and Space Administration Langley Research Center Hampton, Virginia[removed] Add to Reading List Source URL: www.nasa.gov Language: English - Date: 2013-04-30 16:58:18 Dynamics Wind tunnels Langley Research Center Airspeed National Transonic Facility Transonic speed Mach number UTA Aerodynamics Research Center Eight-Foot High Speed Tunnel Aerodynamics Aerospace engineering Fluid dynamics
114	1- by 1-Foot Supersonic Wind Tunnel at NASA Glenn Research Center Add to Reading List Source URL: www.grc.nasa.gov Language: English - Date: 2011-11-07 08:48:34 Dynamics Jet engines Airspeed Spacecraft propulsion Rocket-based combined cycle Hypersonic speed Supersonic wind tunnel Wind tunnel Mach number Aerospace engineering Aerodynamics Fluid dynamics
115	Calibration of the 11-By 11-Foot Transonic Wind Tunnel at the NASA Ames Research Center Max A. Amaya* and Alan R. Boone† NASA Ames Research Center, Moffett Field, CA A series of calibration and flow survey tests were Add to Reading List Source URL: www.nasa.gov Language: English - Date: 2013-12-26 11:13:41 Aerospace engineering Dynamics Aircraft instruments Measuring instruments Dimensionless numbers Wind tunnel Pressure measurement Pressure coefficient Mach number Aerodynamics Fluid dynamics Fluid mechanics
116	NASA AMES UNITARY PLAN WIND TUNNEL BLOCKAGE RECOMMENDATIONS Ames does not have specific criteria to which users of our facilities must adhere. However, the following suggestions are offered to users of our wind tunnels: Add to Reading List Source URL: www.nasa.gov Language: English - Date: 2013-12-26 11:13:41 Dynamics Fluid mechanics Wind tunnel National Advisory Committee for Aeronautics Swept wing Ames Research Center Drag Mach number Transonic speed Aerodynamics Aerospace engineering Fluid dynamics
117	National Aeronautics and Space Administration NASA’s Aeronautics Test Program 10- by 10-Foot Supersonic Wind Tunnel Add to Reading List Source URL: facilities.grc.nasa.gov Language: English - Date: 2011-10-20 07:04:33 Space technology Dynamics Spacecraft propulsion Jet engines Supersonic wind tunnel Unstart Wind tunnel Rocket engine Mach number Aerospace engineering Aerodynamics Fluid dynamics
118	National Aeronautics and Space Administration NASA’s Aeronautics Test Program 10- by 10-Foot Supersonic Wind Tunnel Add to Reading List Source URL: www.grc.nasa.gov Language: English - Date: 2011-10-20 07:04:33 Space technology Dynamics Spacecraft propulsion Jet engines Supersonic wind tunnel Unstart Wind tunnel Rocket engine Mach number Aerospace engineering Aerodynamics Fluid dynamics
119	<7265762E3320454E5F81798E518D6C817A835E834382C689A28F4282CC4449908488DA5F322E392E786C7378> Add to Reading List Source URL: www.meti.go.jp Language: English - Date: 2013-01-06 02:54:04 Mach Physics Aerodynamics Airspeed Mach number
120	AIAA[removed]AIAA SciTech[removed]January 2014, National Harbor, Maryland AIAA Atmospheric Flight Mechanics Conference An Analytical Approach to Modeling Supersonic Add to Reading List Source URL: www.ssdl.gatech.edu Language: English - Date: 2014-01-25 15:05:06 Aerodynamics Plume Shock wave Bow shock Aerodynamic drag Mach number Nozzle Oblique shock Lift Fluid dynamics Fluid mechanics Dynamics

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